DC Field | Value | Language |
---|---|---|
dc.contributor.author | 윤형주 | ko |
dc.contributor.author | 신효상 | ko |
dc.contributor.author | 탁민제 | ko |
dc.date.accessioned | 2013-03-06T18:26:08Z | - |
dc.date.available | 2013-03-06T18:26:08Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2008-11 | - |
dc.identifier.citation | 한국항공우주학회지, v.36, no.11, pp.1072 - 1078 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/87947 | - |
dc.description.abstract | An adaptive control algorithm for spacecraft rendezvous and docking in a Keplerian orbit is presented. The equations of relative motion of two spacecrafts expressed in a local-vertical-local-horizontal rectangular frame are converted to a general Hamiltonian form, then an adaptive control method developed for the uncertain Hamiltonian system is applied to the rendezvous and docking problem. A smooth projection algorithm is applied to keep the parameter estimates inside a singularity-free region, and a numerical example shows that the developed controller successfully deals with the unknown mass of the chaser spacecraft. | - |
dc.language | Korean | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | 우주비행체의 랑데부 및 도킹을 위한 적응 제어기법 | - |
dc.title.alternative | Adaptive Tracking Control for Spacecraft Rendezvous and Docking | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 36 | - |
dc.citation.issue | 11 | - |
dc.citation.beginningpage | 1072 | - |
dc.citation.endingpage | 1078 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.contributor.localauthor | 탁민제 | - |
dc.contributor.nonIdAuthor | 윤형주 | - |
dc.contributor.nonIdAuthor | 신효상 | - |
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